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[texts]Extended tables of stiffness and carry-over factor for structural members under axial load - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806524&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Design and construction; Aerodynamics--Research
Downloads: 198
[texts]Index of NACA technical publications (Volume 1915-1949) - United States: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF030392191&ix=pm&I=0&V=D&pm=1
Keywords: Aeronautics--Abstracts
Downloads: 551
[texts]Application of spring tabs to elevator controls - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613162&ix=nu&I=0&V=D&pm=1
Keywords: Flutter (Aerodynamics; Elevators (Airplanes; Aerodynamics--Research
Downloads: 97
[texts]Performance of basic XJ79-GE-1 turbojet engine and its components - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003852967&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Turbojet engines
Downloads: 202
[texts]Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638506%26ix=nu%26I=0%26V=D%26pm=1
Keywords: Mach number; Aerofoils; Drag (Aerodynamics; Lift (Aerodynamics; Aerodynamics--Research; Aerodynamics--Research
Downloads: 535
[texts]Determination of the stress concentration factor of a stepped shaft stressed in torsion by means of precision strain gages - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003760230&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Torsion; Strains and stresses--Research
Downloads: 236
[texts]Boundary layers in fluids with little friction : = Grenzschichten in flüssigkeiten mit kleiner reibung - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003690109&ix=nu&I=0&V=D&pm=1
Keywords: Aeronautics; Turbulent boundary layer
Downloads: 190
[texts]Flat plate cascades at supersonic speed - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807842&ix=nu&I=0&V=D&pm=1
Keywords: Cascades (Fluid dynamics; Aerodynamics--Research
Downloads: 80
[texts]Research abstracts (Volume no.17(1952:Feb.19)) - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF030398287&ix=pm&I=0&V=D&pm=1
Keywords: Aeronautics
Downloads: 62
[texts]Monthly list of documents released by the NACA during .. (Volume 288(1951:Mar.)) - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF030954133&ix=pm&I=0&V=D&pm=1
Keywords: Aeronautics
Downloads: 69
[texts]Stresses around rectangular cut-outs in skin-stringer panels under axial loads - II - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806425&ix=nu&I=0&V=D&pm=1
Keywords: Strains and stresses; Aerodynamics--Research
Downloads: 110
[texts]Note on compressibility effects on downwash at the tail at subcritical speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003617581&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 118
[texts]Numerical evaluation of the wake-survey equations for subsonic flow including the effect of energy addition - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003624211&ix=nu&I=0&V=D&pm=1
Keywords: Wakes (Aerodynamics; Aeronautics--Research
Downloads: 354
[texts]Wind-tunnel investigation of NACA 66(215)-216, 66,1-212, and 651-212 airfoils with 0.20-airfoil-chord split flaps - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003622093&ix=nu&I=0&V=D&pm=1
Keywords: Flaps (Airplanes; Aerofoils; Aerodynamics--Research
Downloads: 119
[texts]Preliminary investigation of supersonic diffusers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638287&ix=nu&I=0&V=D&pm=1
Keywords: Diffusers; Aerodynamics, Supersonic
Downloads: 168
[texts]Concerning the flow about ring-shaped cowlings.: Part II, Annular bodies of infinite length with circulation for smooth entrance - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779492&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Motors--Cowlings
Downloads: 162
[texts]Development of cowling for long-nose air-cooled engine in the NACA full-scale wind tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805104&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Motors--Cowlings; Aerodynamics--Research
Downloads: 97
[texts]On the theory of the turbulent boundary layer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778607&ix=nu&I=0&V=D&pm=1
Keywords: Aeronautics; Turbulent boundary layer
Downloads: 102
[texts]Research abstracts /National Advisory Committee for Aeronautics (Volume no.68(1954:Aug.17))
http://uf.catalog.fcla.edu/uf.jsp?st=UF001469326
Keywords: Aeronautics Abstracts Periodicals
Downloads: 76
[texts]Effect of variation in diameter and pitch of rivets on compressive strength of panels with z-section stiffeners.: I, panels with close stiffener spacing that fail by local buckling - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638639&ix=nu&I=0&V=D&pm=1
Keywords: Rivets and riveting, Aircraft; Aerodynamics--Research
Downloads: 97
[texts]Research abstracts (Volume no.27(1952:Aug.3)) - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF030398287&ix=pm&I=0&V=D&pm=1
Keywords: Aeronautics
Downloads: 44
[texts]Heat transmission in the boundary layer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003759949&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulent boundary layer
Downloads: 110
[texts]Lift on a bent, flat plate - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778991&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Wings
Downloads: 201
[texts]Air-water analogy and the study of hydraulic models - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778929&ix=nu&I=0&V=D&pm=1
Keywords: Aeronautics; Hydraulic models
Downloads: 93
[texts]Method of quadrature for calculation of the laminar and turbulent boundary layer in case of plane and rotationally symmetrical flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807714&ix=nu&I=0&V=D&pm=1
Keywords: Laminar boundary layer--Research; Aerodynamics--Research
Downloads: 88
[texts]Wind-tunnel investigation of a rectangular NACA 2212 airfoil with semispan ailerons and with nonperforated, balanced double split flaps for use as aerodynamic brakes - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614467&ix=nu&I=0&V=D&pm=1
Keywords: Flaps (Airplanes; Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 257
[texts]Research abstracts /National Advisory Committee for Aeronautics (Volume no.69(1954:Sept.7))
http://uf.catalog.fcla.edu/uf.jsp?st=UF001469326
Keywords: Aeronautics Abstracts Periodicals
Downloads: 88
[texts]Problem of slip flow in aerodynamics - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853242&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Air flow
Downloads: 208
[texts]Determination of induced velocity in front of an inclined propeller by a magnetic-analogy method - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003596963&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aeronautics--Research
Downloads: 154
[texts]Calculation of stick forces for an elevator with a spring tab - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613059&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 128
[texts]Research abstracts (Volume no.35(1953:Jan.5)) - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF030398287&ix=pm&I=0&V=D&pm=1
Keywords: Aeronautics
Downloads: 59
[texts]Research abstracts (Volume no.19(1952:Mar.19)) - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF030398287&ix=pm&I=0&V=D&pm=1
Keywords: Aeronautics
Downloads: 45
[texts]Propellers in yaw - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805565&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Yawing (Aerodynamics; Aeronautics--Research
Downloads: 136
[texts]NACA impact basin and water landing tests of a float model at various velocities and weights - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804832&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 126
[texts]NACA mach number warning device for use in flight - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804356&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Aerodynamics
Downloads: 139
[texts]Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806616&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 118
[texts]Concerning the flow about ring-shaped cowlings of finite thickness: Part I - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779497&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Motors--Cowlings
Downloads: 68
[texts]Numerical evaluation by harmonic analysis of the epsilon-function of the Theodorsen arbitrary-airfoil potential theory - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003595904&ix=nu&I=0&V=D&pm=1
Keywords: Conformal mapping; Harmonic analysis; Aeronautics--Research
Downloads: 104
[texts]On the contribution of turbulent boundary layers to the noise inside a fuselage - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874415&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulent boundary layer--Research; Airplanes--Fuselage
Downloads: 68
[texts]Calculation of turbulent expansion processes - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780797&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulent boundary layer
Downloads: 90
[texts]Some effects of heat transfer at Mach number 2.0 at stagnation temperatures between 2,310° and 3,500° R on a magnesium fin with several leading-edge modifications - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853254&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research; Magnesium--Electrometallurgy
Downloads: 101
[texts]Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808495&ix=nu&I=0&V=D&pm=1
Keywords: Afterburners--Research; Aerodynamics--Research
Downloads: 71
[texts]Some experiences regarding the nonlinearity of hot wires - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003760215&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Heat--Transmission
Downloads: 64
[texts]Effect of wing modifications on the longitudinal stability of a tailless all-wing airplane model - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616165&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 122
[texts]Investigations of the boundary-layer control on a full scale swept wing with air bled off from the turbojet - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875541&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Turbojet engines--Research; Airplanes--Wings, Swept-back; Boundary layer
Downloads: 192
[texts]Solution of the laminar-boundary-layer equation for the flat plate for velocity and temperature fields for variable physical properties and for the diffusion field at high concentration : = Über die lösung der laminaren grenzschichtgleichung an der ebenen platte für geschwindigkeits- und temperaturfeld bei veränderlichen stoffwerten und für das diffusionsfeld bei höheren konzentrationen - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003689761&ix=nu&I=0&V=D&pm=1
Keywords: Boundary layer; Laminar flow
Downloads: 124
[texts]Effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614166&ix=nu&I=0&V=D&pm=1
Keywords: Yawing (Aerodynamics; Aerodynamics--Research
Downloads: 187
[texts]Wire cloth as porous material for transpiration-cooled walls - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810642&ix=nu&I=0&V=D&pm=1
Keywords: Wire screens; Airplanes--Motors--Cooling; Aerodynamics--Research
Downloads: 153
[texts]Flow of gas through turbine lattices - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807492&ix=nu&I=0&V=D&pm=1
Keywords: Cascades (Fluid dynamics; Aerodynamics--Research
Downloads: 102
[texts]Effect of compressibility on the hovering performance of two 10-foot-diameter helicopter rotors tested in the Langley full-scale tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834396&ix=nu&I=0&V=D&pm=1
Keywords: Rotors (Helicopters; Aerodynamics--Research
Downloads: 107
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